NASA has certified the current version of the SpaceX Falcon 9 to launch some categories of science missions, a milestone needed for the upcoming, but delayed, launch of an astronomy spacecraft.
SpaceNews.com

The U.S. Air Force and Aerojet Rocketdyne are working to revise an agreement to support development of the company's AR1 rocket engine, as questions continue about the engine's long-term future.
SpaceNews.com

The president of the Canadian Space Agency said he is taking a "wait and see" approach to NASA's plans to end funding of the International Space Station in the mid-2020s, citing the lack of detail.
SpaceNews.com

NASA’s topline budget will be flat for the foreseeable future — which means an effective decrease in real dollar funding for the agency. As a result, President Trump may see his moon plans come crashing down to Earth.
SpaceNews.com

Satellite hardware and network builder Gilat of Israel, seeking to interest cellular operators in expanding their reach by satellite, is pressing forward with a strategy of building the entire network for them in exchange for multi-year commitments to pay for the service.
SpaceNews.com

The Trump administration is offering $19.6 billion for NASA in its fiscal year 2019 request, while seeking to cancel a flagship astronomy mission and end NASA funding of the International Space Station in 2025.
SpaceNews.com

NASA's fiscal year 2019 budget proposal will include plans to end funding for the International Space Station in 2025, but leaves open the possibility of handing part or all of the station over to private operators.
SpaceNews.com

Intelligent and team-oriented Aerospace Engineer with a strong educational background and proven talent through numerous notable projects applying extensive mathematical, design and computer knowledge. Expertise with the interpretation of technical engineering specifics and flexible and pro-active support of flight engineering and operational procedures. Able to analyze and strategize from a group perspective and streamline solutions with clarity and enthusiasm.

EDUCATION

Master of Science in Aerospace Engineering | San Jose State University | San Jose, CA (GPA 3.2/4.0) – 2012

Modeled a projectile and composite plate in HYPERMESH. Kevlar 29–epoxy and Kevlar 49–epoxy materials, 2-d shell elements were used for modeling. The edges of the plate were fixed. AK-47 bullet was used as the projectile. The steel bullet was modeled with 2-d solid elements and input with a projectile velocity of 700 m/s. The stress/failure analysis was performed on the composite plate at five different ply orientation angles using the ABAQUS solver

Analysis of Ribs and Spars of an Aircraft Wing

Ribs and spars of a two-seater general aviation aircraft were designed in CATIA and stress analysis was performed in MSC NASTRAN/PATRAN. The shape of the rib was based on an NACA 0012 airfoil. The rib structure was optimized; cut-outs and flanges were optimized based on the stress analysis results. An I-beam spar was used to provide concentration to key loading points and due to maximum bending resistance to weight ratio

Design, Manufacture and Analysis of a Finite Wing

A finite wing was constructed with wood out of an NACA 23018 airfoil with no sweep. Wind tunnel tests were performed on the wing at different angles of attack. The results were compared with the CFD results

Design, Manufacture and Analysis of an Aircraft with Maximum Payload Capabilities

A model aircraft with maximum payload capabilities was designed and constructed using wood. A surface flow visualization was performed in a low speed wind tunnel with a flow speed of 30 m/s. Flow data was measured using pivot tubes that were set up throughout the surface of the model and compared with the CFD results obtained from GAMBIT/FLUENT

Sonic Boom Mitigation by Aircraft Nose Cone Modification

The sonic boom intensities of five different axisymmetric aircraft nose geometries were studied through analytical method and CFD analysis. The nose geometry was modeled using SOLID WORKS. The CFD analysis was performed using ESI CFD to find geometries of lesser deflection angles producing a relatively lesser sonic boom

CFD Analysis of Airflow within the Front Wheel Cavity of Automobiles

2-d and 3-d flow analyses of front wheel cavity of a car were performed using GAMBIT/FLUENT with a rotating boundary condition specified for the wheel. Results indicated drag produced is proportional to the size of the cavity

Design of a 4-Seat General Aviation Electric Aircraft

Designed a 4-seat general aviation electric aircraft with a maximum range of 800 Km. The aircraft is powered by an electric power system that comprises of a battery driven electric motor-propeller system. The aircraft has a takeoff weight of 1750 kg, and a cruise speed of 200 km/hr

Design of an Aerial Firefighting Vehicle

Designed an aerial firefighting vehicle that will replace the fleet of aircraft currently in operation. It is a twin engine amphibious aircraft with a twin tail boom empennage that is designed to carry a payload of 12,500 lbs. This will enable the aircraft to carry 1,200 gallons of water or fire retardant

CFD Analysis of a Subsonic Joined Wing Aircraft

A joined wing aircraft was modeled in SOLID WORKS. The analysis was performed using ESI CFD in 3 stages; wing tips, wings and interaction between wing and fuselage. The results were obtained to verify increased aerodynamic performance, increased wing structure support, high maneuverability and STOL ability

CAD Design & Analysis Projects – CATIA V5

* Harley Davidson wheel design

* Motorized can crusher – Design, Motion Analysis and Optimization

* Machine Gun – Design, Motion Analysis, FEA and Optimization

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